N957LR

Part: NONE — NONE · airframe 14,982 hrs · 11,290 cycles

FWD FA FLASHLIGHT NOT BLINKING. PLACED ON MEL.

Part: BATTERY PACK — UNSECURE (ZONE 200) · airframe 14,363 hrs · 10,877 cycles

ROW 12 LWR LVL EXIT SIGNS INOP RESECURED #3 BATT PACK & CHARGED BATTS

Part: SKIN — DENTED (FS485.0-FS501.0) · airframe 13,686 hrs · 10,384 cycles

FWD FUSELAGE SKIN PANEL BETWEEN FS485.0 -FS501.0, STGR23R -STGR24R WAS FOUND TO HAVE A DENT. PERFOMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-31-01-001-003-A02, ITEM 1, 53-31-01-101-003-A04, EA81-2021-074.

Part: ACCESS PANEL — CORRODED (LT WING LE) · airframe 13,686 hrs · 10,384 cycles

LH WING LEADING EDGE ACCESS PANEL (522CB) BETWEEN SS 99.68 & SS 111.922 WAS FOUND WITH WEAR DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 57-42-32, 57-42-32-991-801, ITEM 9D, EA 72-2021-069. DEFECT LOCATION: LH W1NG LEADING EDGE/ SS 99.68 & SS 111.922

Part: SKIN — DENTED (FS1051-1069) · airframe 13,686 hrs · 10,384 cycles

AFT FUSELAGE SKIN PANEL BETWEEN FS1051.30 -FS1069.75, STGR18R -STGR19R WAS FOUND TO HAVE A DENT. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-60-01-001-004-A02, ITEMS 1F AND G, EA 84-2021-001.

Part: SLAT TRACK — CORRODED (RT WING) · airframe 13,686 hrs · 10,384 cycles

SLAT TRACK 1-1 OF SLAT #1 ON THE RH WING WAS FOUND TO HAVE CORROSION DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 IPC 27-81-41, FIGURE 1, ITEM 45, EA 69-2021-148.

Part: ANTENNA — DAMAGED (ELT) · airframe 13,686 hrs · 10,384 cycles

EMERGENCY LOCATOR TRANSPONDER ANTENNA WAS FOUND TO HAVE DAMAGED AND MISSING PAINT OVER THE MAJORITY OF ITS SURFACE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 AIPC 25-62-01, FIGURE 1B, ITEM 5, EA 12-2021-216.

Part: SKIN — WORN (RT COWL) · airframe 13,686 hrs · 10,384 cycles

RH ENGINE CORE COWL WAS FOUND TO HAVE EDGE WEAR DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 54-13-01, FIGURE 54-13-01-991-801, ITEM 1, EA 72-2021-151.

Part: SKIN — NICKED (BS 1000 -1031) · airframe 13,686 hrs · 10,384 cycles

FUSELAGE SKIN BETWEEN FS1000.00 & FS1031.00 AND STGR22R & STGR24R WAS FOUND TO HAVE SEVERAL NICKS. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-61-01, FIGURE 53-61-01-991-806, ITEM 1D, EA 69-2021-136.

Part: SKIN — DENTED (BS 295-319) · airframe 13,686 hrs · 10,384 cycles

LOWER FUSELAGE SKIN PANEL BETWEEN FS295 -FS319 & STGR23L -STGR27 WAS FOUND TO HAVE TWO DENTS. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-21-01-001-002-A01, ITEMS 1 AND E, EA 69-2021-140

Part: FLOORBEAM — CRACKED (BS 280 RBL 12) · airframe 13,686 hrs · 10,384 cycles

COCKPIT FLOOR BEAM AT FS 280, RBL 12.00 WAS FOUND WITH CRACK DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-11-43, FIGURE 53-11-43-991-801 ITEM 109D, EA 72-2021-146.

Part: DOOR — DENTED (RT NACELLE) · airframe 13,686 hrs · 10,384 cycles

OUTER SKIN PANEL OF THE LOWER RH FAN COWL DOOR WAS FOUND TO HAVE 3 DENTS AT 4 O'CLOCK AND 8 O'CLOCK POSITIONS. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 54-14-00-101-001-A01 ,"FAN COWL DOORS -ALLOWABLE DAMAGE", EA 69-2021-139.

Part: SLAT TRACK — CORRODED (RT WING) · airframe 13,686 hrs · 10,384 cycles

SLAT TRACK 1-3 OF SLAT #1 ON THE RH WING WAS FOUND TO HAVE CORROSION DAMAGE ON THE UPPER FACE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 IPC 27-81-41, FIGURE 1, ITEM 105, EA 69-2021-150.

Part: DUCT — TORN (CABIN AIR) · airframe 13,686 hrs · 10,384 cycles

FWD CABIN DISTRIBUTION DUCT WAS FOUND TO HAVE TEAR DAMAGE AFFECTING THE INSULATION BLANKET. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 IPC 21-23-51, FIGURE 1, ITEM 5, EA 69-2021-143.

Part: SLAT TRACK — CORRODED (LT WING) · airframe 13,686 hrs · 10,384 cycles

SLAT TRACK 2-2 OF SLAT #2 ON THE LH AND RH WING WAS FOUND TO HAVE CORROSION DAMAGE ON THE LOWER FACE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 IPC 27-81-41, FIGURE 5, ITEM 85, EA 69-2021-152.

Part: PLATE — CORRODED (BS 557) · airframe 13,686 hrs · 10,384 cycles

FORWARD BAGGAGE BAY PLATE AT LBL3.4 AND FS557 WAS FOUND TO HAVE MINOR CORROSION. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-32-58-001-001-A02, FIGURE 53-32-58-991-802, ITEM 109, EA 79-2021-217.

Part: DRAIN — DENTED (LAV TOILET) · airframe 13,686 hrs · 10,384 cycles

FORWARD LAVATORY UPPER TOILET DRAIN WAS FOUND TO HAVE A DENT WITH WEAR DAMAGE TO THE OUTER INSULATION. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 AIPC 38-31-19, FIGURE 5B, ITEM 5, EA 12-2021-212. DEFECT LOCATION: OUTER INSULATION ADJ TO THE BEND IN THE DRAIN

Part: FLOORBEAM — CRACKED (BS 280 LBL 12.) · airframe 13,686 hrs · 10,384 cycles

COCKPIT FLOOR BEAM AT FS 280, LBL 12.00 WAS FOUND WITH CRACK DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-11-43, FIGURE 53-11-43-991-801 ITEM 108G , EA 72-2021-145.

Part: SKIN — DAMAGED (BS 288-295) · airframe 13,686 hrs · 10,384 cycles

FUSELAGE SKIN AT FS288.00 - FS295.00 BETWEEN STGR17R - STGR18R WAS FOUND TO HAVE AN UNDOCUMENTED BLENDOUT. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-21-01, FIGURE 53-21-01-991-802, ITEM 1 , EA 72-2021-144.

Part: SLAT TRACK — CORRODED (LT WING) · airframe 13,686 hrs · 10,384 cycles

SLAT TRACK 1-2 OF SLAT #1 ON THE LH AND RH WINGS WAS FOUND TO HAVE CORROSION DAMAGE ON THE LOWER FACE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 IPC 27-81-41, FIGURE 1, ITEM 85, EA 69-2021-149.

Part: SLAT TRACK — CORRODED (RT WING) · airframe 13,686 hrs · 10,384 cycles

SLAT TRACK 2-1 OF SLAT #2 ON THE RH WING WAS FOUND TO HAVE CORROSION DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 IPC 27-81-41, FIGURE 5, ITEM 15, EA 69-2021-151.

Part: SLAT TRACK — CORRODED (RT WING) · airframe 13,686 hrs · 10,384 cycles

SLAT TRACK 2-3 OF SLAT #2 ON THE RH WING WAS FOUND TO HAVE CORROSION DAMAGE ON THE UPPER FACE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 IPC 27-81-41, FIGURE 5, ITEM 105, EA 69-2021-153.

Part: DUCT — DAMAGED (AIR DISTRBUTION) · airframe 13,686 hrs · 10,384 cycles

AFT CARGO COMPARTMENT AIR DISTRIBUTION DUCT WAS FOUND TO HAVE TEAR DAMAGE AFFECTING THE INSULATION BLANKET. PERFORMED PERMANENT REPAIR JAW CRJ 700/900 AMM 25-80-00-340-803, "REPAIR THE INSULATION BLANKET (BA6XX -457XX), EA 20-2021-169.

Part: SKIN — CORRODED (BS 280-290) · airframe 13,686 hrs · 10,354 cycles

CORROSION WAS REPORTED AFFECTING INNER FUSELAGE SKIN BETWEEN FS280-290 AND STGRS 25R-24R AT THE MAIN AVIONICS COMPARTMENT. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-21-01-001-002-A01, ITEM 1, EA 81-2021-069.

Part: SUPPORT — CORRODED (BS 265 S26L-R) · airframe 13,686 hrs · 10,384 cycles

CORROSION ON SUPPORTS OF NOSE JACKING SUPPORT STRUCTURE BETWEEN FS265.00 - FS280.00 AND STGR26L - STGR26R JACKING SUPPORTS WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01

Part: ANGLE — CORRODED (FUSELAGE) · airframe 13,686 hrs · 10,384 cycles

CORROSION WAS FOUND ON INNER FACE OF STIFFENING ANGLE | STIFFENING ANGLE WAS REPLACE PER ETL-900-21-080.REV. ORIGINAL AND EA-QRO-MR-072

Part: STRINGER — DAMAGED (BS 280-319 S17) · airframe 13,686 hrs · 10,384 cycles

DURING REPAIR OF LOWER SILL BTW FS 280-FS 319 BTW RBL 40-42 IN REF NRC S/N 00277, STRINGER 17 WAS DRILLED BTW FS 280-282 APPROX. STRINGER 17 BTW FS 280-FS 319 RH WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND SR M51-42-21-001-001-A01.

Part: RIB — CRACKED (RT WING LE) · airframe 13,686 hrs · 10,384 cycles

CRACK ON RIB LEADING EDGE SS57.16 AT RIGHT WING LEADING EDGE, WAS REPAIRED PER REO #690-57-41-240 REV.-

Part: DUCT — TORN (AIR DISTRBUTION) · airframe 13,686 hrs · 10,384 cycles

AFT CARGO COMPARTMENT AIR DISTRIBUTION DUCT WAS FOUND TO HAVE TEAR DAMAGE AFFECTING THE INSULATION BLANKET. PERFORMED PERMANENT REPAIR CRJ 700/900 IAW AMM 25-80-00-340-803 "REPAIR OF THE INSULATION BLANKET" (BA6XX-457XX).

Part: SKIN — DENTED (BS 1051-1069) · airframe 13,686 hrs · 10,384 cycles

FUSELAGE SKIN PANEL BETWEEN FS1051.30-FS1069.75, STGR18R-STGR19R WAS FOUND TO HAVE DENTS. PERFORMED PERMANENT REPAIR IAW CRJ700/900 SRM 53-60-01-001-004-A02, ITEMS 1F AND G, EA 84-2021-001.

Part: SKIN — DAMAGED (BS1000-1031) · airframe 13,686 hrs · 10,384 cycles

FUSELAGE SKIN BETWEEN FS1000.00- FS1031.00 & STGR22R - STGR24R WAS FOUND TO HAVE SEVERAL NICKS. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-61-01, FIGURE 53-61-01-991-806, ITEM 1D, EA 69-2021-136. DEFECT LOCATION: FUSELAGE/FS 1000,00-FS1031.00 & STGR.22R-STGR2.4R

Part: PLATE — CORRODED (BS 557 LBL3) · airframe 13,686 hrs · 10,384 cycles

FORWARD BAGGAGE BAY PLATE AT LBL3.4 AND FS557 WAS FOUND TO HAVE MINOR CORROSION DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-32-58-001-001-A02, FIGURE 53-32-58-991-802, ITEM 109, EA 79-2021-217.

Part: SKIN — DAMAGED (BS 288-295) · airframe 13,686 hrs · 10,384 cycles

FUSELAGE SKIN AT FS288.00-FS295.00 BETWEEN STGR17R-STGR18R WAS FOUND TO HAVE AN UNDOCUMENTED BLENDOUT. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-21-01, FIGURE 53-21-01-991-802, ITEM 1, EA 72-2021-144. DEFECT LOCATION: FUSELAGE FS288.00-FS295.00 & STGR17R-STGR18R

Part: FLOORBEAM — CRACKED (BS 280 LBL 12) · airframe 13,686 hrs · 10,384 cycles

CRACK ON FLOOR BEAM LBL 12.00, FS280.00, WL73.5 AT FWD AVIONICS/FLIGHT CONTROLS COMPARTMENT. FLOOR BEAM LBL 12.00, FS280.00, WL73.5 WAS REPAIRED PER EA 72-2021-145 REV. IR

Part: SUPPORT — CORRODED (BS 280-319) · airframe 13,686 hrs · 10,384 cycles

CORROSION AT LOWER SILL BTW FS 280 AND FS 319 AND BTW RBL 40 AND RBL 42. LOWER SILL BTW FS 280 AND FS 319 AND BTW RBL 40 AND RBL 42 WAS REPAIRED PER CRJ900 SRM 53-00-45-201-001-A01

Part: STRINGER — CORRODED (BS 265 S26R) · airframe 13,686 hrs · 10,384 cycles

CORROSION WAS FOUND ON STGR26R AND FS265.00 AT FWD AVIONICS |STGR26R AND FS265.00 AT FWD AVIONICS WAS REPAIRED CRJ900 SRM 53-00-03-201-001-A02

Part: CANISTER — CRACKED (LT FUEL TANK) · airframe 13,686 hrs · 10,384 cycles

CRACK IN CANISTER, WELDED NO.3 IN STA. WS148 AT LH MAIN FUEL TANK. CANISTER, WELDED NO.3 IN STA. WS148 AT LH MAIN FUEL TANK WAS REPAIRED PER REO 670-57-42-577 REV. --

Part: CANISTER — CRACKED (RT FUEL TANK) · airframe 13,686 hrs · 10,384 cycles

CRACK IN CANISTER, WELDED NO.3 IN STA. WS148 AT RH MAIN FUEL TANK. CANISTER, WELDED NO.3 IN STA. WS148 AT RH MAIN FUEL TANK WAS REPAIRED PER REO 670-57-42-577 REV. --

Part: FLOORBEAM — CRACKED (BS 280 RBL 12) · airframe 13,686 hrs · 10,384 cycles

CRACK ON FLOOR BEAM RBL 12.00, FS280.00, WL73.5 AT FWD AVIONICS/FLIGHT CONTROLS COMPARTMENT. FLOOR BEAM RBL 12.00, FS280.00, WL73.5 WAS REPAIRED PER EA 72-2021-146 REV. IR

Part: SEAT TRACK — DAMAGED (BS 364-477) · airframe 13,686 hrs · 10,384 cycles

NICKS ON SIDE SE AT RAIL FROM FS364.00 TO FS477.40 ON STGR 15LH. NEW SIDE SE AT RAIL FROM FS364.00 TO FS477.40 ON STGR 15LH WAS INSTALLED PER CRJ 900 AMM 53-00-49-400-801 (CONFIG A12)

Part: SEAT TRACK — CORRODED (BS 785-847) · airframe 13,686 hrs · 10,384 cycles

CORROSION ON SIDE SEAT RAIL FROM FS785.15 TO FS847.00 ON STGR 15LH AND STGR 15RH. NEW SIDE SE AT RAIL FROM FS785.15 TO FS847.00 ON STGR 15LH AND STGR 15RH WERE INSTALLED PER CRJ-900 AMM 53-00-49-400-801 (CONFIG A12)

Part: DOUBLER — CRACKED (ACCESS FWD) · airframe 13,686 hrs · 10,384 cycles

CRACK IN DOUBLER BELOW OF ADG RESTOW PUMP AT FWD EQUIPMENT COMPARTMENT STRUCTURE DOUBLER BELOW OF ADG RESTOW PUMP AT FWD EQUIPMENT COMPARTMENT STRUCTURE WAS REPAIRED PER CRJ 900 SRM 53-11-43-201-001-A01

Part: STRINGER — CORRODED (E/E BAY) · airframe 13,686 hrs · 10,384 cycles

CORROSION ON STGR 26R BTW FS280-319 AT MAIN AVIONICS COMPARTMENT. STRINGER 26RH BTW FS=280 TO FS=333 WAS REPLACED FOR A NEW ONE PER CRJ900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01

Part: SEAT TRACK — CORRODED (BS 349-477) · airframe 13,686 hrs · 10,384 cycles

CORROSION ON SEAT REAIL FROM FS349.00 TO FS477.40 AT RBL9 | NEW SEAT RAIL FROM FS 349.00 TO FS477.40 AT RBL 9.00 WAS INSTALLED PER CRJ-900 AMM 53-00-49

Part: STRINGER SPLICE — CORRODED (BS 333 S25R) · airframe 13,686 hrs · 10,384 cycles

CORROSION ON SPLICE STGR 25R AT FS333, MAIN AVIONICS COMPARTMENT. NEW STRINGER SPLICE FS=333 STRG 25RH WAS INSTALLED PER CRJ900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01

Part: INTERCOSTAL — CORRODED (BS 349-364 S26L) · airframe 13,686 hrs · 10,384 cycles

CORROSION ON INTERCOSTALS {3EAS) BTW FS349-364 AND STGR 26L-26R AT MAIN AVIONICS COMPARTMENT. CORROSION WAS REMOVED ON INTERCOSTAL BTW FS 349-364 AT STGR 26R AND REWORKED AREA WAS MEASURE AND WAS FOUND WITHIN LIMITS PER CRJ 900 SRM 53-21-23-101-003-A02. INTERCOSTAL (2 EAS) BTW FS 349-FS 364 AT STGR 27 WERE REPLACED PER CRJ 900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01.

Part: SKIN — CORRODED (BS 280-295) · airframe 13,686 hrs · 10,384 cycles

CORROSION ON INNER FUSELAGE SKIN BTW FS280-295 STGR 25R-24R AT MAIN AVIONICS COMPARTMENT. FUSELAGE SKIN BTW FS280-295 STGR 25R-24R WAS REPAIRED PER EA 81-2021-069 REV. A

Part: STRINGER — CORRODED (BS 295-319 S25R) · airframe 13,686 hrs · 10,384 cycles

CORROSION ON STGR 25R BTW FS295-319 AT MAIN AVIONICS COMPARTMENT. NEW STRINGER 25RH BTW FS=280 TO FS=333 WAS INSTALLED PER CRJ900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01

Part: SEAT TRACK — CORRODED (BS 897-942) · airframe 13,686 hrs · 10,384 cycles

CORROSION ON SIDE SEAT RAIL FROM FS897.70 TO FS942.00 ON STGR 15LH. SECTION SIDE SEAT RAIL FROM FS897.70 TO FS942.00 ON STGR 15LH WAS REPLACED PER CRJ/900 AMM 53-00-49-400-801 (CONFIG. 12).

Part: SEAT TRACK — CORRODED (BS 744-761) · airframe 13,686 hrs · 10,384 cycles

CORROSION ON SIDE SEAT RAIL FROM FS744.15 TO FS761.85 ON STGR 15LH AND STGR 15RH. NEW SIDE SEAT RAIL FROM FS744.15 TO FS761.85 ON STGR 15LH AND STGR 15RH WERE INSTALLED PER CRJ-900 AMM 53-00-49-400-801 (CONFIG A 12)

Part: INTERCOSTAL — CORRODED (BS 310-333 S20R) · airframe 13,686 hrs · 10,384 cycles

CORROSION ON INTERCOSTAL AND ANGLES ATTACHED TO STGR 20RH IN STA. FS= 310 TO FS= 333 AT MAIN AVIONICS COMPARTMENT. INTERCOSTAL AND ANGLES ATTACHED TO STGR 20RH IN STA. FS= 310 TO FS= 333 AT MAIN AVIONICS COMPARTMENT WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 PAR.6.C.

Part: STRINGER SPLICE — CORRODED (BS 333 S24R) · airframe 13,686 hrs · 10,384 cycles

CORROSION ON SPLICE STGR 24R AT FS333, MAIN AVIONICS COMPARTMENT. STRINGER SPLICE 24RH AT FS=333 WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01

Part: INTERCOSTAL — CORRODED (BS 333-349 S20R) · airframe 13,686 hrs · 10,384 cycles

CORROSION ON INTERCOSTAL AND ANGLES ATTACHED TO STRINGER 20RH IN STA. FS= 333 TO FS= 349. INTERCOSTAL WAS REPLACED PER CRJ/900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01 AND ANGLES WERE EVALUATED AND WERE FOUND WITHIN LIMITS PER CRJ-900 SRM 53-21-23-101-002-A02

Part: SKIN — DAMAGED (LT WING TE FLAP) · airframe 13,686 hrs · 10,384 cycles

DENTS AND NICKS IN STA. BL= 45 TO WS= 48 ON INBD FLAP LOWER SKIN AT LH WING DENTS AND NICKS WERE REPAIRED PER EA 80-2021-131 REV. IR

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,197 hrs · 10,030 cycles

SVC DOOR AFT LOWER EMERG FLOOD LIGHT INOP- PLACED ON MEL

Part: CONNECTOR — UNSECURE (BRAKE OVERHEAT) · airframe 12,440 hrs · 9,532 cycles

BRAKE OVERHEAT WARNING IN FLIGHT, RESECURED BRAKE TEMP CONNECTOR.

Part: BATTERY PACK — INOPERATIVE (AFT FLASHLIGHT) · airframe 12,101 hrs · 9,278 cycles

AFT FA FLASHLIGHT INOPERABLE. REPLACED BATTERY.

Part: SHIMMY DAMPENER — DAMAGED (LT MLG) · airframe 11,632 hrs · 8,916 cycles

THE LT MLG SHIMMY DAMPER CAME APART ON LANDING CAUSING THE MLG TO TURN SLIGHTLY AND UPPER TORQUE LINK CAME IN CONTACT WITH THE NUMBER 2 MLG TIRE CAUSING TIRE TO BURST. A/C IN PROCCESS OF LH MLG REPLACEMENT.

Part: A/C PACK — SMOKE (ZONE 200) · airframe 10,719 hrs · 8,244 cycles

SMOKE AND FUMES AFT CABIN TROUBLE SHOT TO RT PACK AND PLACED ON MEL

Part: LIGHT — INOPERATIVE (RT OVERWING) · airframe 8,012 hrs · 6,093 cycles

RH AFT EXT OVWNG EMERG LIGHT INOP. PLACED ON MEL

Part: HINGE — GOUGED (PAX DOOR) · airframe 5,687 hrs · 4,434 cycles

PASSENGER DOOR HINGE 232ND LUG FROM FRONT ON DOOR SIDE IS GOUGED.

Part: BATTERY — DISCHARGED (CABIN) · airframe 2,119 hrs · 1,661 cycles

EMERGENCY LIGHTS WOULD NOT STAY ON. CHARGED BATTERIES.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 1,592 hrs · 1,258 cycles

EMERGENCY LIGHTS WILL NOT STAY ON. CHARGED BATTERIES.